GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 460 AIRFOIL (goe460-il) Reynolds number: 200,000 Max Cl/Cd: 46.41 at α=9.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe460-il-200000.txt Download as CSV file: xf-goe460-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 460 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0724 0.08839 0.08230 -0.0636 1.0000 0.0791
-19.500 -1.0727 0.08546 0.07932 -0.0645 1.0000 0.0807
-19.250 -1.0790 0.08173 0.07547 -0.0657 1.0000 0.0825
-19.000 -1.0890 0.07759 0.07114 -0.0670 1.0000 0.0841
-18.750 -1.0896 0.07481 0.06829 -0.0675 1.0000 0.0859
-18.500 -1.0830 0.07297 0.06650 -0.0676 1.0000 0.0878
-18.250 -1.0833 0.07026 0.06374 -0.0681 1.0000 0.0900
-18.000 -1.0876 0.06712 0.06046 -0.0687 1.0000 0.0921
-17.750 -1.0953 0.06366 0.05680 -0.0692 1.0000 0.0941
-17.500 -1.0833 0.06257 0.05584 -0.0687 1.0000 0.0967
-17.250 -1.0813 0.06033 0.05357 -0.0687 1.0000 0.0995
-17.000 -1.0839 0.05762 0.05073 -0.0687 1.0000 0.1023
-16.750 -1.0804 0.05564 0.04874 -0.0683 1.0000 0.1055
-16.500 -1.0767 0.05377 0.04691 -0.0678 1.0000 0.1090
-16.250 -1.0783 0.05135 0.04439 -0.0675 1.0000 0.1128
-16.000 -1.0746 0.04954 0.04263 -0.0667 1.0000 0.1171
-15.750 -1.0742 0.04750 0.04059 -0.0660 1.0000 0.1215
-15.500 -1.0763 0.04525 0.03822 -0.0652 1.0000 0.1262
-15.250 -1.0739 0.04354 0.03665 -0.0642 1.0000 0.1312
-15.000 -1.0752 0.04156 0.03458 -0.0631 1.0000 0.1364
-14.750 -1.0743 0.03986 0.03295 -0.0618 1.0000 0.1413
-14.500 -1.0745 0.03820 0.03126 -0.0604 1.0000 0.1464
-14.250 -1.0737 0.03667 0.02966 -0.0588 1.0000 0.1516
-14.000 -1.0731 0.03530 0.02834 -0.0570 1.0000 0.1562
-13.750 -1.0724 0.03402 0.02698 -0.0550 1.0000 0.1615
-13.500 -1.0702 0.03288 0.02583 -0.0529 1.0000 0.1662
-13.250 -1.0687 0.03185 0.02480 -0.0505 1.0000 0.1707
-13.000 -1.0681 0.03088 0.02373 -0.0479 1.0000 0.1759
-12.750 -1.0658 0.02999 0.02283 -0.0452 1.0000 0.1805
-12.500 -1.0649 0.02920 0.02206 -0.0422 1.0000 0.1850
-12.250 -1.0662 0.02846 0.02125 -0.0388 1.0000 0.1902
-12.000 -1.0658 0.02775 0.02050 -0.0353 1.0000 0.1951
-11.750 -1.0659 0.02714 0.01993 -0.0317 1.0000 0.1998
-11.500 -1.0693 0.02659 0.01933 -0.0275 1.0000 0.2049
-11.250 -1.0745 0.02608 0.01872 -0.0228 1.0000 0.2098
-11.000 -1.0744 0.02555 0.01830 -0.0189 1.0000 0.2150
-10.750 -1.0808 0.02516 0.01788 -0.0139 1.0000 0.2200
-10.500 -1.0901 0.02484 0.01745 -0.0083 1.0000 0.2248
-10.250 -1.0908 0.02438 0.01708 -0.0041 1.0000 0.2301
-10.000 -1.0968 0.02407 0.01676 0.0011 1.0000 0.2350
-9.750 -1.1053 0.02384 0.01644 0.0068 1.0000 0.2401
-9.500 -1.0789 0.02337 0.01603 0.0060 0.9962 0.2487
-9.250 -1.0501 0.02314 0.01572 0.0048 0.9914 0.2577
-9.000 -1.0226 0.02266 0.01531 0.0040 0.9859 0.2659
-8.750 -0.9938 0.02244 0.01502 0.0030 0.9807 0.2751
-8.500 -0.9642 0.02205 0.01469 0.0019 0.9758 0.2834
-8.250 -0.9392 0.02178 0.01438 0.0018 0.9691 0.2918
-8.000 -0.9029 0.02141 0.01405 -0.0005 0.9654 0.3004
-7.750 -0.8807 0.02111 0.01376 0.0001 0.9581 0.3079
-7.500 -0.8481 0.02074 0.01338 -0.0012 0.9526 0.3161
-7.250 -0.8091 0.02037 0.01305 -0.0039 0.9493 0.3258
-7.000 -0.7902 0.02005 0.01274 -0.0025 0.9404 0.3341
-6.750 -0.7565 0.01966 0.01240 -0.0039 0.9353 0.3456
-6.500 -0.7169 0.01919 0.01201 -0.0065 0.9322 0.3585
-6.250 -0.7025 0.01891 0.01174 -0.0041 0.9217 0.3705
-6.000 -0.6676 0.01846 0.01133 -0.0056 0.9170 0.3873
-5.750 -0.6274 0.01793 0.01088 -0.0082 0.9142 0.4065
-5.500 -0.6162 0.01766 0.01069 -0.0049 0.9026 0.4205
-5.250 -0.5778 0.01717 0.01026 -0.0070 0.8988 0.4388
-5.000 -0.5345 0.01671 0.00986 -0.0100 0.8964 0.4573
-4.750 -0.5214 0.01653 0.00973 -0.0069 0.8851 0.4706
-4.500 -0.4852 0.01615 0.00937 -0.0084 0.8805 0.4874
-4.250 -0.4456 0.01576 0.00900 -0.0105 0.8772 0.5040
-4.000 -0.4316 0.01564 0.00891 -0.0075 0.8653 0.5162
-3.750 -0.3944 0.01530 0.00861 -0.0091 0.8603 0.5301
-3.500 -0.3703 0.01511 0.00840 -0.0081 0.8516 0.5427
-3.250 -0.3407 0.01486 0.00818 -0.0081 0.8431 0.5545
-3.000 -0.3005 0.01453 0.00785 -0.0103 0.8379 0.5664
-2.750 -0.2859 0.01447 0.00778 -0.0074 0.8252 0.5770
-2.500 -0.2469 0.01418 0.00751 -0.0093 0.8186 0.5879
-2.250 -0.2318 0.01412 0.00741 -0.0066 0.8058 0.5988
-2.000 -0.1934 0.01387 0.00720 -0.0084 0.7983 0.6095
-1.750 -0.1785 0.01381 0.00711 -0.0056 0.7850 0.6206
-1.500 -0.1452 0.01364 0.00698 -0.0063 0.7753 0.6314
-1.250 -0.1239 0.01352 0.00685 -0.0047 0.7623 0.6427
-1.000 -0.0994 0.01343 0.00679 -0.0037 0.7499 0.6540
-0.750 -0.0699 0.01331 0.00665 -0.0037 0.7391 0.6653
-0.500 -0.0522 0.01327 0.00662 -0.0014 0.7260 0.6779
-0.250 -0.0225 0.01324 0.00662 -0.0014 0.7147 0.6895
0.000 0.0000 0.01321 0.00659 0.0000 0.7022 0.7022
0.250 0.0225 0.01324 0.00662 0.0014 0.6896 0.7147
0.500 0.0521 0.01327 0.00662 0.0014 0.6778 0.7259
0.750 0.0700 0.01331 0.00666 0.0037 0.6653 0.7392
1.000 0.0993 0.01343 0.00679 0.0037 0.6541 0.7501
1.250 0.1240 0.01352 0.00686 0.0047 0.6428 0.7624
1.500 0.1451 0.01364 0.00698 0.0063 0.6313 0.7753
1.750 0.1785 0.01381 0.00711 0.0056 0.6206 0.7850
2.000 0.1933 0.01387 0.00719 0.0084 0.6095 0.7982
2.250 0.2318 0.01412 0.00742 0.0066 0.5989 0.8058
2.500 0.2470 0.01418 0.00751 0.0093 0.5880 0.8186
2.750 0.2859 0.01447 0.00778 0.0074 0.5770 0.8252
3.000 0.3006 0.01454 0.00785 0.0103 0.5664 0.8380
3.250 0.3409 0.01487 0.00818 0.0081 0.5546 0.8431
3.500 0.3703 0.01511 0.00839 0.0081 0.5427 0.8515
3.750 0.3945 0.01530 0.00861 0.0090 0.5301 0.8604
4.000 0.4318 0.01564 0.00891 0.0074 0.5165 0.8653
4.250 0.4456 0.01576 0.00900 0.0105 0.5040 0.8772
4.500 0.4852 0.01614 0.00937 0.0084 0.4873 0.8805
4.750 0.5212 0.01652 0.00972 0.0070 0.4707 0.8851
5.000 0.5347 0.01671 0.00986 0.0100 0.4574 0.8964
5.250 0.5779 0.01717 0.01026 0.0070 0.4389 0.8988
5.500 0.6161 0.01766 0.01069 0.0049 0.4205 0.9026
5.750 0.6273 0.01793 0.01087 0.0082 0.4063 0.9142
6.000 0.6675 0.01845 0.01132 0.0057 0.3872 0.9171
6.250 0.7025 0.01891 0.01173 0.0041 0.3705 0.9218
6.500 0.7170 0.01919 0.01201 0.0065 0.3585 0.9322
6.750 0.7566 0.01965 0.01239 0.0039 0.3454 0.9354
7.000 0.7905 0.02005 0.01274 0.0024 0.3341 0.9405
7.250 0.8095 0.02036 0.01304 0.0038 0.3257 0.9493
7.500 0.8484 0.02074 0.01338 0.0012 0.3161 0.9526
7.750 0.8809 0.02111 0.01375 -0.0002 0.3079 0.9581
8.000 0.9032 0.02140 0.01404 0.0004 0.3004 0.9654
8.250 0.9396 0.02177 0.01438 -0.0019 0.2917 0.9691
8.500 0.9646 0.02204 0.01468 -0.0020 0.2833 0.9758
8.750 0.9943 0.02243 0.01502 -0.0031 0.2751 0.9808
9.000 1.0231 0.02266 0.01530 -0.0041 0.2659 0.9859
9.250 1.0499 0.02312 0.01571 -0.0048 0.2575 0.9915
9.500 1.0793 0.02336 0.01602 -0.0061 0.2485 0.9963
9.750 1.1054 0.02382 0.01643 -0.0068 0.2401 1.0000
10.000 1.0967 0.02405 0.01674 -0.0011 0.2349 1.0000
10.250 1.0907 0.02437 0.01706 0.0041 0.2300 1.0000
10.500 1.0904 0.02483 0.01743 0.0082 0.2248 1.0000
10.750 1.0806 0.02514 0.01786 0.0139 0.2199 1.0000
11.000 1.0744 0.02553 0.01828 0.0189 0.2150 1.0000
11.250 1.0745 0.02606 0.01870 0.0228 0.2098 1.0000
11.500 1.0693 0.02657 0.01931 0.0275 0.2049 1.0000
11.750 1.0660 0.02711 0.01990 0.0317 0.1998 1.0000
12.000 1.0659 0.02773 0.02048 0.0353 0.1950 1.0000
12.250 1.0659 0.02844 0.02123 0.0388 0.1900 1.0000
12.500 1.0654 0.02917 0.02203 0.0422 0.1850 1.0000
12.750 1.0661 0.02996 0.02280 0.0452 0.1804 1.0000
13.000 1.0684 0.03085 0.02371 0.0479 0.1757 1.0000
13.250 1.0695 0.03182 0.02476 0.0505 0.1707 1.0000
13.500 1.0707 0.03286 0.02579 0.0528 0.1660 1.0000
13.750 1.0729 0.03400 0.02696 0.0549 0.1613 1.0000
14.000 1.0738 0.03526 0.02830 0.0569 0.1561 1.0000
14.250 1.0749 0.03662 0.02960 0.0587 0.1515 1.0000
14.500 1.0755 0.03816 0.03122 0.0603 0.1462 1.0000
14.750 1.0756 0.03981 0.03288 0.0617 0.1413 1.0000
15.000 1.0765 0.04151 0.03452 0.0630 0.1364 1.0000
15.250 1.0754 0.04348 0.03659 0.0640 0.1311 1.0000
15.500 1.0781 0.04516 0.03812 0.0651 0.1261 1.0000
15.750 1.0760 0.04742 0.04051 0.0659 0.1214 1.0000
16.000 1.0764 0.04947 0.04254 0.0665 0.1170 1.0000
16.250 1.0804 0.05126 0.04429 0.0673 0.1127 1.0000
16.500 1.0787 0.05368 0.04682 0.0676 0.1089 1.0000
16.750 1.0825 0.05557 0.04866 0.0681 0.1055 1.0000
17.000 1.0868 0.05747 0.05057 0.0685 0.1023 1.0000
17.250 1.0836 0.06024 0.05348 0.0684 0.0994 1.0000
17.500 1.0859 0.06245 0.05572 0.0685 0.0967 1.0000
17.750 1.0988 0.06344 0.05656 0.0690 0.0939 1.0000
18.000 1.0894 0.06711 0.06046 0.0684 0.0920 1.0000
18.250 1.0853 0.07025 0.06372 0.0678 0.0898 1.0000
18.500 1.0860 0.07284 0.06636 0.0673 0.0878 1.0000
18.750 1.0925 0.07468 0.06816 0.0672 0.0858 1.0000
19.000 1.0917 0.07752 0.07107 0.0667 0.0840 1.0000
19.250 1.0816 0.08168 0.07542 0.0654 0.0824 1.0000
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